Methods and systems for dual fuel injection

ABSTRACT

Methods and systems are provided for reducing fueling errors resulting from pressure pulsations in a port injection fuel rail. The pressure pulsations result from pressure pulsations generated in a high pressure fuel pump delivering fuel to both the port injection fuel rail and a direct injection fuel rail. A center of a port injection fuel pulse is positioned on an average pressure-crossing of the pressure pulsations so as to cancel out the effect of the over-average and under-average pressure pulsations.

CROSS REFERENCE TO RELATED APPLICATION

The present application claims priority to U.S. Provisional Patent Application No. 62/175,059, entitled “Methods and Systems for Dual Fuel Injection,” filed on Jun. 12, 2015, the entire contents of which are hereby incorporated by reference for all purposes.

FIELD

The present description relates to systems and methods for adjusting operation of an internal combustion engine that includes high pressure port and direct fuel injectors.

BACKGROUND AND SUMMARY

Direct fuel injection (DI) systems provide some advantages over port fuel injection systems. For example, direct fuel injection systems may improve cylinder charge cooling so that engine cylinders may operate at higher compression ratios without incurring undesirable engine knock. However, direct fuel injectors may not be able to provide a desired amount of fuel to a cylinder at higher engine speeds and loads because the amount of time a cylinder stroke takes is shortened so that there may not be sufficient time to inject a desired amount of fuel. Consequently, the engine may develop less power than is desired at higher engine speeds and loads. In addition, direct injection systems may be more prone to particulate matter emissions.

In an effort to reduce the particulate matter emissions and fuel dilution in oil, very high pressure direct injection systems have been developed. For example, while nominal direct injection maximum pressures are in the range of 150 bar, the higher pressure DI systems may operate in the range of 250-800 bar using a high pressure piston pump that is mechanically driven by the engine via a camshaft. In engines configured with dual injection systems, that is engines enabled with both direct and port fuel injectors, pressurized fuel from the fuel tank may be supplied to both the direct injection high pressure fuel pump (HPFP) as well as the port injection fuel rail. In order to reduce hardware complexity, the fuel may be supplied to the port injection fuel rail either through the HPFP, or may be branched off before the pump, thereby reducing the need for a dedicated pump for the port injection fuel rail.

However, one issue with such dual fuel injection system configurations is that fuel pulsations from the high pressure fuel pump may enter the port injection fuel rail. This is due to the sinusoidal fuel pressure generated at the high pressure fuel pump due to the pump being driven by the engine via a camshaft (and cam lobes). The pulsations may worsen when the HPFP is not flowing any fuel into the direct injection fuel rail (such as when direct injection is disabled) due to the pump returning all of the ingested volume back into the low pressure region of the fuel system. The pulsations in the port injection fuel rail can lead to larger discrepancies between the value of rested fuel in the port injection fuel rail as compared to value of fuel injected from the port injection fuel rail. As such, this can result in large fueling errors.

In one example, the above issue may be at least partly addressed by a method for an engine, comprising: pressurizing fuel in a port injection fuel rail via an engine camshaft driven high pressure fuel pump; and injecting a port fuel injection with a timing balanced around an average pressure-crossing of port fuel injection pressure. In this way, fueling errors due to fuel pump induced pressure fluctuations in the port injection fuel rail are reduced.

As one example, an engine system may include an engine-driven high pressure fuel pump supplying fuel to each of a port and direct injection fuel rail. The fuel pump may be a piston pump coupled to the engine via each of a camshaft and cam lobes, and due to this configuration, the fuel pressure in the fuel pump may vary in a sinusoidal manner. This may in turn cause sinusoidal fluctuations in a fuel pressure in the port injection fuel rail. An engine controller may estimate the pressure in the port injection fuel rail based on the pressure at the fuel pump, and further based on an engine speed dependent fuel pulse delay. The controller may estimate the timing (with respect to engine position) of local maxima and local minima in the waveform of the port injection fuel rail pressure, and accordingly determine the position of zero-crossings of the waveform. An initial timing and width of a port fuel injection pulse may be determined based on engine operating conditions including, for example, intake valve opening (IVO) and fuel flow velocity through the fuel system to allow for a closed intake valve injection. The timing of the port injection fuel pulse may then be moved to coincide with the timing of a first zero-crossing in the advanced direction. In addition, the initial pulse width of the port injection fuel pulse may be adjusted based on the adjusted timing to compensate for any difference in fuel puddle dynamics.

The technical effect of centering a port fuel injection pulse around a zero-crossing of a fuel rail pressure waveform is that under-average pressure changes can be cancelled out by over-average pressure changes. By moving the middle of injection angle of the port injection fuel pulse to coincide with an average pressure at the first zero-crossing in the advanced direction, closed intake valve port fuel injection can be maintained while port injection fuel rail pressure fluctuations induced by sinusoidal changes in a fuel pump pressure are substantially removed. By relying on the average port injection fuel rail pressure, the need for fast fuel pressure sampling is reduced. In addition, pressure fluctuations can be addressed without requiring additional pressure dampeners, check valves, or orifices. Overall, metering of fuel from the port injection fuel rail is improved while removing the need for a dedicated fuel line for the port injection fuel system.

It should be understood that the summary above is provided to introduce in simplified form a selection of concepts that are further described in the detailed description. It is not meant to identify key or essential features of the claimed subject matter, the scope of which is defined uniquely by the claims that follow the detailed description. Furthermore, the claimed subject matter is not limited to implementations that solve any disadvantages noted above or in any part of this disclosure.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 schematically depicts an example embodiment of a cylinder of an internal combustion engine.

FIG. 2 schematically depicts an example embodiment of a fuel system configured for high pressure port injection and high pressure direct injection that may be used with the engine of FIG. 1.

FIG. 3 depicts alternate embodiments of a dual fuel injection system that may be used with the engine of FIG. 1.

FIG. 4 shows a flow chart of a method for adjusting a timing of a port fuel injection pulse based on an average pressure-crossing of a port injection fuel rail pressure.

FIG. 5 shows an example of aligning fuel injection pulse timing with a zero-crossing of a port injection fuel rail pressure waveform.

FIG. 6A depicts an example relationship between port injection fuel rail pressure and fuel pressure at a high pressure fuel pump delivering fuel to the port injection fuel rail.

FIG. 6B depicts an example relationship between fuel pulse delay and engine speed.

DETAILED DESCRIPTION

The following detailed description provides information regarding a high pressure fuel pump and a system for reducing high pressure pump-induced pressure fluctuations at a port injection fuel rail. An example embodiment of a cylinder in an internal combustion engine is given in FIG. 1 while FIGS. 2-3 depict example fuel systems that may be used with the engine of FIG. 1. A controller may be configured to perform a control routine, such as the example routine of FIG. 4, to reposition a port injection fuel pulse so as to align a center of the fuel pulse with an average port injection fuel rail pressure. The port injection fuel rail pressure may be estimated based on fuel pump pressure and engine speed (FIGS. 6A-6B). An example repositioning of a port fuel injection pulse is shown at FIG. 5.

Regarding terminology used throughout this detailed description, a high pressure pump, or direct injection pump, may be abbreviated as a DI or HP pump. Similarly, a low pressure pump, or lift pump, may be abbreviated as a LP pump. Port fuel injection may be abbreviated as PFI while direct injection may be abbreviated as DI. Also, fuel rail pressure, or the value of pressure of fuel within a fuel rail, may be abbreviated as FRP. Also, the mechanically operated inlet check valve for controlling fuel flow into the HP pump may also be referred to as the spill valve. As discussed in more detail below, an HP pump that relies on mechanical pressure regulation without use of an electronically-controlled inlet valve may be referred to as a mechanically-controlled HP pump, or HP pump with mechanically-regulated pressure. Mechanically-controlled HP pumps, while not using electronically-controlled inlet valves for regulating a volume of fuel pumped, may provide one or more discrete pressures based on electronic selection.

FIG. 1 depicts an example of a combustion chamber or cylinder of internal combustion engine 10. Engine 10 may be controlled at least partially by a control system including controller 12 and by input from a vehicle operator 130 via an input device 132. In this example, input device 132 includes an accelerator pedal and a pedal position sensor 134 for generating a proportional pedal position signal PP. Cylinder (herein also “combustion chamber”) 14 of engine 10 may include combustion chamber walls 136 with piston 138 positioned therein. Piston 138 may be coupled to crankshaft 140 so that reciprocating motion of the piston is translated into rotational motion of the crankshaft. Crankshaft 140 may be coupled to at least one drive wheel of the passenger vehicle via a transmission system. Further, a starter motor (not shown) may be coupled to crankshaft 140 via a flywheel to enable a starting operation of engine 10.

Cylinder 14 can receive intake air via a series of intake air passages 142, 144, and 146. Intake air passage 146 can communicate with other cylinders of engine 10 in addition to cylinder 14. In some examples, one or more of the intake passages may include a boosting device such as a turbocharger or a supercharger. For example, FIG. 1 shows engine 10 configured with a turbocharger including a compressor 174 arranged between intake passages 142 and 144, and an exhaust turbine 176 arranged along exhaust passage 148. Compressor 174 may be at least partially powered by exhaust turbine 176 via a shaft 180 where the boosting device is configured as a turbocharger. However, in other examples, such as where engine 10 is provided with a supercharger, exhaust turbine 176 may be optionally omitted, where compressor 174 may be powered by mechanical input from a motor or the engine. A throttle 162 including a throttle plate 164 may be provided along an intake passage of the engine for varying the flow rate and/or pressure of intake air provided to the engine cylinders. For example, throttle 162 may be positioned downstream of compressor 174 as shown in FIG. 1, or alternatively may be provided upstream of compressor 174.

Exhaust passage 148 can receive exhaust gases from other cylinders of engine 10 in addition to cylinder 14. Exhaust gas sensor 128 is shown coupled to exhaust passage 148 upstream of emission control device 178. Sensor 128 may be selected from among various suitable sensors for providing an indication of exhaust gas air/fuel ratio such as a linear oxygen sensor or UEGO (universal or wide-range exhaust gas oxygen), a two-state oxygen sensor or EGO (as depicted), a HEGO (heated EGO), a NOx, HC, or CO sensor, for example. Emission control device 178 may be a three way catalyst (TWC), NOx trap, various other emission control devices, or combinations thereof.

Each cylinder of engine 10 may include one or more intake valves and one or more exhaust valves. For example, cylinder 14 is shown including at least one intake poppet valve 150 and at least one exhaust poppet valve 156 located at an upper region of cylinder 14. In some examples, each cylinder of engine 10, including cylinder 14, may include at least two intake poppet valves and at least two exhaust poppet valves located at an upper region of the cylinder.

Intake valve 150 may be controlled by controller 12 via actuator 152. Similarly, exhaust valve 156 may be controlled by controller 12 via actuator 154. During some conditions, controller 12 may vary the signals provided to actuators 152 and 154 to control the opening and closing of the respective intake and exhaust valves. The position of intake valve 150 and exhaust valve 156 may be determined by respective valve position sensors (not shown). The valve actuators may be of the electric valve actuation type or cam actuation type, or a combination thereof. The intake and exhaust valve timing may be controlled concurrently or any of a possibility of variable intake cam timing, variable exhaust cam timing, dual independent variable cam timing or fixed cam timing may be used. Each cam actuation system may include one or more cams and may utilize one or more of cam profile switching (CPS), variable cam timing (VCT), variable valve timing (VVT) and/or variable valve lift (VVL) systems that may be operated by controller 12 to vary valve operation. For example, cylinder 14 may alternatively include an intake valve controlled via electric valve actuation and an exhaust valve controlled via cam actuation including CPS and/or VCT. In other examples, the intake and exhaust valves may be controlled by a common valve actuator or actuation system, or a variable valve timing actuator or actuation system.

Cylinder 14 can have a compression ratio, which is the ratio of volumes when piston 138 is at bottom center to top center. In one example, the compression ratio is in the range of 9:1 to 10:1. However, in some examples where different fuels are used, the compression ratio may be increased. This may happen, for example, when higher octane fuels or fuels with higher latent enthalpy of vaporization are used. The compression ratio may also be increased if direct injection is used due to its effect on engine knock.

In some examples, each cylinder of engine 10 may include a spark plug 192 for initiating combustion. Ignition system 190 can provide an ignition spark to combustion chamber 14 via spark plug 192 in response to spark advance signal SA from controller 12, under select operating modes. However, in some embodiments, spark plug 192 may be omitted, such as where engine 10 may initiate combustion by auto-ignition or by injection of fuel as may be the case with some diesel engines.

In some examples, each cylinder of engine 10 may be configured with one or more fuel injectors for providing fuel thereto. As a non-limiting example, cylinder 14 is shown including two fuel injectors 166 and 170. Fuel injectors 166 and 170 may be configured to deliver fuel received from fuel system 8. As elaborated with reference to FIGS. 2 and 3, fuel system 8 may include one or more fuel tanks, fuel pumps, and fuel rails. Fuel injector 166 is shown coupled directly to cylinder 14 for injecting fuel directly therein in proportion to the pulse width of signal FPW-1 received from controller 12 via electronic driver 168. In this manner, fuel injector 166 provides what is known as direct injection (hereafter referred to as “DI”) of fuel into combustion cylinder 14. While FIG. 1 shows injector 166 positioned to one side of cylinder 14, it may alternatively be located overhead of the piston, such as near the position of spark plug 192. Such a position may improve mixing and combustion when operating the engine with an alcohol-based fuel due to the lower volatility of some alcohol-based fuels. Alternatively, the injector may be located overhead and near the intake valve to improve mixing. Fuel may be delivered to fuel injector 166 from a fuel tank of fuel system 8 via a high pressure fuel pump, and a fuel rail. Further, the fuel tank may have a pressure transducer providing a signal to controller 12.

Fuel injector 170 is shown arranged in intake passage 146, rather than in cylinder 14, in a configuration that provides what is known as port injection of fuel (hereafter referred to as “PFI”) into the intake port upstream of cylinder 14. Fuel injector 170 may inject fuel, received from fuel system 8, in proportion to the pulse width of signal FPW-2 received from controller 12 via electronic driver 171. Note that a single driver 168 or 171 may be used for both fuel injection systems, or multiple drivers, for example driver 168 for fuel injector 166 and driver 171 for fuel injector 170, may be used, as depicted.

In an alternate example, each of fuel injectors 166 and 170 may be configured as direct fuel injectors for injecting fuel directly into cylinder 14. In still another example, each of fuel injectors 166 and 170 may be configured as port fuel injectors for injecting fuel upstream of intake valve 150. In yet other examples, cylinder 14 may include only a single fuel injector that is configured to receive different fuels from the fuel systems in varying relative amounts as a fuel mixture, and is further configured to inject this fuel mixture either directly into the cylinder as a direct fuel injector or upstream of the intake valves as a port fuel injector. As such, it should be appreciated that the fuel systems described herein should not be limited by the particular fuel injector configurations described herein by way of example.

Fuel may be delivered by both injectors to the cylinder during a single cycle of the cylinder. For example, each injector may deliver a portion of a total fuel injection that is combusted in cylinder 14. Further, the distribution and/or relative amount of fuel delivered from each injector may vary with operating conditions, such as engine load, knock, and exhaust temperature, such as described herein below. The port injected fuel may be delivered during an open intake valve event, closed intake valve event (e.g., substantially before the intake stroke), as well as during both open and closed intake valve operation. Similarly, directly injected fuel may be delivered during an intake stroke, as well as partly during a previous exhaust stroke, during the intake stroke, and partly during the compression stroke, for example. As such, even for a single combustion event, injected fuel may be injected at different timings from the port and direct injector. Furthermore, for a single combustion event, multiple injections of the delivered fuel may be performed per cycle. The multiple injections may be performed during the compression stroke, intake stroke, or any appropriate combination thereof.

As described above, FIG. 1 shows only one cylinder of a multi-cylinder engine. As such, each cylinder may similarly include its own set of intake/exhaust valves, fuel injector(s), spark plug, etc. It will be appreciated that engine 10 may include any suitable number of cylinders, including 2, 3, 4, 5, 6, 8, 10, 12, or more cylinders. Further, each of these cylinders can include some or all of the various components described and depicted by FIG. 1 with reference to cylinder 14.

Fuel injectors 166 and 170 may have different characteristics. These include differences in size, for example, one injector may have a larger injection hole than the other. Other differences include, but are not limited to, different spray angles, different operating temperatures, different targeting, different injection timing, different spray characteristics, different locations etc. Moreover, depending on the distribution ratio of injected fuel among injectors 170 and 166, different effects may be achieved.

Fuel tanks in fuel system 8 may hold fuels of different fuel types, such as fuels with different fuel qualities and different fuel compositions. The differences may include different alcohol content, different water content, different octane, different heats of vaporization, different fuel blends, and/or combinations thereof etc. One example of fuels with different heats of vaporization could include gasoline as a first fuel type with a lower heat of vaporization and ethanol as a second fuel type with a greater heat of vaporization. In another example, the engine may use gasoline as a first fuel type and an alcohol containing fuel blend such as E85 (which is approximately 85% ethanol and 15% gasoline) or M85 (which is approximately 85% methanol and 15% gasoline) as a second fuel type. Other feasible substances include water, methanol, a mixture of alcohol and water, a mixture of water and methanol, a mixture of alcohols, etc.

In still another example, both fuels may be alcohol blends with varying alcohol composition wherein the first fuel type may be a gasoline alcohol blend with a lower concentration of alcohol, such as E10 (which is approximately 10% ethanol), while the second fuel type may be a gasoline alcohol blend with a greater concentration of alcohol, such as E85 (which is approximately 85% ethanol). Additionally, the first and second fuels may also differ in other fuel qualities such as a difference in temperature, viscosity, octane number, etc. Moreover, fuel characteristics of one or both fuel tanks may vary frequently, for example, due to day to day variations in tank refilling.

Controller 12 is shown in FIG. 1 as a microcomputer, including microprocessor unit 106, input/output ports 108, an electronic storage medium for executable programs and calibration values shown as non-transitory read only memory chip 110 in this particular example for storing executable instructions, random access memory 112, keep alive memory 114, and a data bus. Controller 12 may receive various signals from sensors coupled to engine 10, in addition to those signals previously discussed, including measurement of inducted mass air flow (MAF) from mass air flow sensor 122; engine coolant temperature (ECT) from temperature sensor 116 coupled to cooling sleeve 118; a profile ignition pickup signal (PIP) from Hall effect sensor 120 (or other type) coupled to crankshaft 140; throttle position (TP) from a throttle position sensor; and absolute manifold pressure signal (MAP) from sensor 124. Engine speed signal, RPM, may be generated by controller 12 from signal PIP. Manifold pressure signal MAP from a manifold pressure sensor may be used to provide an indication of vacuum, or pressure, in the intake manifold. The controller 12 receives signals from the various sensors of FIG. 1 (and FIG. 2) and employs the various actuators of FIG. 1 (and FIG. 2) to adjust engine operation based on the received signals and instructions stored on a memory of the controller

FIG. 2 schematically depicts an example embodiment 200 of a fuel system, such as fuel system 8 of FIG. 1. Fuel system 200 may be operated to deliver fuel to an engine, such as engine 10 of FIG. 1. Fuel system 200 may be operated by a controller to perform some or all of the operations described with reference to the process flows of FIGS. 4 and 6A-6B.

Fuel system 200 includes a fuel storage tank 210 for storing the fuel on-board the vehicle, a lower pressure fuel pump (LPP) 212 (herein also referred to as fuel lift pump 212), and a higher pressure fuel pump (HPP) 214 (herein also referred to as fuel injection pump 214). Fuel may be provided to fuel tank 210 via fuel filling passage 204. In one example, LPP 212 may be an electrically-powered lower pressure fuel pump disposed at least partially within fuel tank 210. LPP 212 may be operated by a controller 222 (e.g., controller 12 of FIG. 1) to provide fuel to HPP 214 via fuel passage 218. LPP 212 can be configured as what may be referred to as a fuel lift pump. As one example, LPP 212 may be a turbine (e.g., centrifugal) pump including an electric (e.g., DC) pump motor, whereby the pressure increase across the pump and/or the volumetric flow rate through the pump may be controlled by varying the electrical power provided to the pump motor, thereby increasing or decreasing the motor speed. For example, as the controller reduces the electrical power that is provided to lift pump 212, the volumetric flow rate and/or pressure increase across the lift pump may be reduced. The volumetric flow rate and/or pressure increase across the pump may be increased by increasing the electrical power that is provided to lift pump 212. As one example, the electrical power supplied to the lower pressure pump motor can be obtained from an alternator or other energy storage device on-board the vehicle (not shown), whereby the control system can control the electrical load that is used to power the lower pressure pump. Thus, by varying the voltage and/or current provided to the lower pressure fuel pump, the flow rate and pressure of the fuel provided at the inlet of the higher pressure fuel pump 214 is adjusted.

LPP 212 may be fluidly coupled to a filter 217, which may remove small impurities contained in the fuel that could potentially damage fuel handling components. A check valve 213, which may facilitate fuel delivery and maintain fuel line pressure, may be positioned fluidly upstream of filter 217. With check valve 213 upstream of the filter 217, the compliance of low-pressure passage 218 may be increased since the filter may be physically large in volume. Furthermore, a pressure relief valve 219 may be employed to limit the fuel pressure in low-pressure passage 218 (e.g., the output from lift pump 212). Relief valve 219 may include a ball and spring mechanism that seats and seals at a specified pressure differential, for example. The pressure differential set-point at which relief valve 219 may be configured to open may assume various suitable values; as a non-limiting example the set-point may be 6.4 bar or 5 bar (g). An orifice 223 may be utilized to allow for air and/or fuel vapor to bleed out of the lift pump 212. This bleed at 223 may also be used to power a jet pump used to transfer fuel from one location to another within the tank 210. In one example, an orifice check valve (not shown) may be placed in series with orifice 223. In some embodiments, fuel system 8 may include one or more (e.g., a series) of check valves fluidly coupled to low-pressure fuel pump 212 to impede fuel from leaking back upstream of the valves. In this context, upstream flow refers to fuel flow traveling from fuel rails 250, 260 towards LPP 212 while downstream flow refers to the nominal fuel flow direction from the LPP towards the HPP 214 and thereon to the fuel rails.

Fuel lifted by LPP 212 may be supplied at a lower pressure into a fuel passage 218 leading to an inlet 203 of HPP 214. HPP 214 may then deliver fuel into a first fuel rail 250 coupled to one or more fuel injectors of a first group of direct injectors 252 (herein also referred to as a first injector group). Fuel lifted by the LPP 212 may also be supplied to a second fuel rail 260 coupled to one or more fuel injectors of a second group of port injectors 262 (herein also referred to as a second injector group). As elaborated below, HPP 214 may be operated to raise the pressure of fuel delivered to each of the first and second fuel rail above the lift pump pressure, with the first fuel rail coupled to the direct injector group operating with a variable high pressure while the second fuel rail coupled to the port injector group operates with a fixed high pressure. As a result, high pressure port and direct injection may be enabled. The high pressure fuel pump is coupled downstream of the low pressure lift pump with no additional pump positioned in between the high pressure fuel pump and the low pressure lift pump.

While each of first fuel rail 250 and second fuel rail 260 are shown dispensing fuel to four fuel injectors of the respective injector group 252, 262, it will be appreciated that each fuel rail 250, 260 may dispense fuel to any suitable number of fuel injectors. As one example, first fuel rail 250 may dispense fuel to one fuel injector of first injector group 252 for each cylinder of the engine while second fuel rail 260 may dispense fuel to one fuel injector of second injector group 262 for each cylinder of the engine. Controller 222 can individually actuate each of the port injectors 262 via a port injection driver 237 and actuate each of the direct injectors 252 via a direct injection driver 238. The controller 222, the drivers 237, 238 and other suitable engine system controllers can comprise a control system. While the drivers 237, 238 are shown external to the controller 222, it should be appreciated that in other examples, the controller 222 can include the drivers 237, 238 or can be configured to provide the functionality of the drivers 237, 238. Controller 222 may include additional components not shown, such as those included in controller 12 of FIG. 1.

HPP 214 may be an engine-driven, positive-displacement pump. As one non-limiting example, HPP 214 may be a BOSCH HDP5 HIGH PRESSURE PUMP, which utilizes a solenoid activated control valve (e.g., fuel volume regulator, magnetic solenoid valve, etc.) 236 to vary the effective pump volume of each pump stroke. The outlet check valve of HPP is mechanically controlled and not electronically controlled by an external controller. HPP 214 may be mechanically driven by the engine in contrast to the motor driven LPP 212. HPP 214 includes a pump piston 228, a pump compression chamber 205 (herein also referred to as compression chamber), and a step-room 227. Pump piston 228 receives a mechanical input from the engine crank shaft or cam shaft via cam 230, thereby operating the HPP according to the principle of a cam-driven single-cylinder pump. A sensor (not shown in FIG. 2) may be positioned near cam 230 to enable determination of the angular position of the cam (e.g., between 0 and 360 degrees), which may be relayed to controller 222.

Fuel system 200 may optionally further include accumulator 215. When included, accumulator 215 may be positioned downstream of lower pressure fuel pump 212 and upstream of higher pressure fuel pump 214, and may be configured to hold a volume of fuel that reduces the rate of fuel pressure increase or decrease between fuel pumps 212 and 214. For example, accumulator 215 may be coupled in fuel passage 218, as shown, or in a bypass passage 211 coupling fuel passage 218 to the step-room 227 of HPP 214. The volume of accumulator 215 may be sized such that the engine can operate at idle conditions for a predetermined period of time between operating intervals of lower pressure fuel pump 212. For example, accumulator 215 can be sized such that when the engine idles, it takes one or more minutes to deplete pressure in the accumulator to a level at which higher pressure fuel pump 214 is incapable of maintaining a sufficiently high fuel pressure for fuel injectors 252, 262. Accumulator 215 may thus enable an intermittent operation mode (or pulsed mode) of lower pressure fuel pump 212. By reducing the frequency of LPP operation, power consumption is reduced. In other embodiments, accumulator 215 may inherently exist in the compliance of fuel filter 217 and fuel passage 218, and thus may not exist as a distinct element.

A lift pump fuel pressure sensor 231 may be positioned along fuel passage 218 between lift pump 212 and higher pressure fuel pump 214. In this configuration, readings from sensor 231 may be interpreted as indications of the fuel pressure of lift pump 212 (e.g., the outlet fuel pressure of the lift pump) and/or of the inlet pressure of higher pressure fuel pump. Readings from sensor 231 may be used to assess the operation of various components in fuel system 200, to determine whether sufficient fuel pressure is provided to higher pressure fuel pump 214 so that the higher pressure fuel pump ingests liquid fuel and not fuel vapor, and/or to minimize the average electrical power supplied to lift pump 212. While lift pump fuel pressure sensor 231 is shown as being positioned downstream of accumulator 215, in other embodiments the sensor may be positioned upstream of the accumulator.

First fuel rail 250 includes a first fuel rail pressure sensor 248 for providing an indication of direct injection fuel rail pressure to the controller 222. Likewise, second fuel rail 260 includes a second fuel rail pressure sensor 258 for providing an indication of port injection fuel rail pressure to the controller 222. An engine speed sensor 233 can be used to provide an indication of engine speed to the controller 222. The indication of engine speed can be used to identify the speed of higher pressure fuel pump 214, since the pump 214 is mechanically driven by the engine 202, for example, via the crankshaft or camshaft.

First fuel rail 250 is coupled to an outlet 208 of HPP 214 along fuel passage 278. In comparison, second fuel rail 260 is coupled to an inlet 203 of HPP 214 via fuel passage 288. A check valve and a pressure relief valve may be positioned between the outlet 208 of the HPP 214 and the first fuel rail. In addition, pressure relief valve 272, arranged parallel to check valve 274 in bypass passage 279, may limit the pressure in fuel passage 278, downstream of HPP 214 and upstream of first fuel rail 250. For example, pressure relief valve 272 may limit the pressure in fuel passage 278 to 200 bar. As such, pressure relief valve 272 may limit the pressure that would otherwise be generated in fuel passage 278 if control valve 236 were (intentionally or unintentionally) open and while high pressure fuel pump 214 were pumping.

One or more check valves and pressure relief valves may also be coupled to fuel passage 218, downstream of LPP 212 and upstream of HPP 214. For example, check valve 234 may be provided in fuel passage 218 to reduce or prevent back-flow of fuel from high pressure pump 214 to low pressure pump 212 and fuel tank 210. In addition, pressure relief valve 232 may be provided in a bypass passage, positioned parallel to check valve 234. Pressure relief valve 232 may limit the pressure to its left to 10 bar higher than the pressure at sensor 231.

Controller 222 may be configured to regulate fuel flow into HPP 214 through control valve 236 by energizing or de-energizing the solenoid valve (based on the solenoid valve configuration) in synchronism with the driving cam. Accordingly, the solenoid activated control valve 236 may be operated in a first mode where the valve 236 is positioned within HPP inlet 203 to limit (e.g., inhibit) the amount of fuel traveling through the solenoid activated control valve 236. Depending on the timing of the solenoid valve actuation, the volume transferred to the fuel rail 250 is varied. The solenoid valve may also be operated in a second mode where the solenoid activated control valve 236 is effectively disabled and fuel can travel upstream and downstream of the valve, and in and out of HPP 214.

As such, solenoid activated control valve 236 may be configured to regulate the mass (or volume) of fuel compressed into the direct injection fuel pump. In one example, controller 222 may adjust a closing timing of the solenoid pressure control check valve to regulate the mass of fuel compressed. For example, a late pressure control valve closing may reduce the amount of fuel mass ingested into compression chamber 205. The solenoid activated check valve opening and closing timings may be coordinated with respect to stroke timings of the direct injection fuel pump.

Pressure relief valve 232 allows fuel flow out of solenoid activated control valve 236 toward the LPP 212 when pressure between pressure relief valve 232 and solenoid operated control valve 236 is greater than a predetermined pressure (e.g., 10 bar). When solenoid operated control valve 236 is deactivated (e.g., not electrically energized), solenoid operated control valve operates in a pass-through mode and pressure relief valve 232 regulates pressure in compression chamber 205 to the single pressure relief set-point of pressure relief valve 232 (e.g., 10 bar above the pressure at sensor 231). Regulating the pressure in compression chamber 205 allows a pressure differential to form from the piston top to the piston bottom. The pressure in step-room 227 is at the pressure of the outlet of the low pressure pump (e.g., 5 bar) while the pressure at piston top is at pressure relief valve regulation pressure (e.g., 15 bar). The pressure differential allows fuel to seep from the piston top to the piston bottom through the clearance between the piston and the pump cylinder wall, thereby lubricating HPP 214.

Piston 228 reciprocates up and down. HPP 214 is in a compression stroke when piston 228 is traveling in a direction that reduces the volume of compression chamber 205. HPP 214 is in a suction stroke when piston 228 is traveling in a direction that increases the volume of compression chamber 205.

A forward flow outlet check valve 274 may be coupled downstream of an outlet 208 of the compression chamber 205. Outlet check valve 274 opens to allow fuel to flow from the high pressure pump outlet 208 into a fuel rail only when a pressure at the outlet of direct injection fuel pump 214 (e.g., a compression chamber outlet pressure) is higher than the fuel rail pressure. Thus, during conditions when direct injection fuel pump operation is not requested, controller 222 may deactivate solenoid activated control valve 236 and pressure relief valve 232 regulates pressure in compression chamber 205 to a single substantially constant pressure during most of the compression stroke. On the intake stroke the pressure in compression chamber 205 drops to a pressure near the pressure of the lift pump (212). Lubrication of DI pump 214 may occur when the pressure in compression chamber 205 exceeds the pressure in step-room 227. This difference in pressures may also contribute to pump lubrication when controller 222 deactivates solenoid activated control valve 236. One result of this regulation method is that the fuel rail is regulated to a minimum pressure, approximately the pressure relief of pressure relief valve 232. Thus, if pressure relief valve 232 has a pressure relief setting of 10 bar, the fuel rail pressure becomes 15 bar because this 10 bar adds to the 5 bar of lift pump pressure. Specifically, the fuel pressure in compression chamber 205 is regulated during the compression stroke of direct injection fuel pump 214. Thus, during at least the compression stroke of direct injection fuel pump 214, lubrication is provided to the pump. When direct fuel injection pump enters a suction stroke, fuel pressure in the compression chamber may be reduced while still some level of lubrication may be provided as long as the pressure differential remains. Another pressure relief valve 272 may be placed in parallel with check valve 274. Pressure relief valve 272 allows fuel flow out of the DI fuel rail 250 toward pump outlet 208 when the fuel rail pressure is greater than a predetermined pressure.

As such, while the direct injection fuel pump is reciprocating, the flow of fuel between the piston and bore ensures sufficient pump lubrication and cooling.

The lift pump may be transiently operated in a pulsed mode where the lift pump operation is adjusted based on a pressure estimated at the outlet of the lift pump and inlet of the high pressure pump. In particular, responsive to high pressure pump inlet pressure falling below a fuel vapor pressure, the lift pump may be operated until the inlet pressure is at or above the fuel vapor pressure. This reduces the risk of the high pressure fuel pump ingesting fuel vapors (instead of fuel) and ensuing engine stall events.

It is noted here that the high pressure pump 214 of FIG. 2 is presented as an illustrative example of one possible configuration for a high pressure pump. Components shown in FIG. 2 may be removed and/or changed while additional components not presently shown may be added to pump 214 while still maintaining the ability to deliver high-pressure fuel to a direct injection fuel rail and a port injection fuel rail.

Solenoid activated control valve 236 may also be operated to direct fuel back-flow from the high pressure pump to one of pressure relief valve 232 and accumulator 215. For example, control valve 236 may be operated to generate and store fuel pressure in accumulator 215 for later use. One use of accumulator 215 is to absorb fuel volume flow that results from the opening of compression pressure relief valve 232. Accumulator 227 sources fuel as check valve 234 opens during the intake stroke of pump 214. Another use of accumulator 215 is to absorb/source the volume changes in the step room 227. Yet another use of accumulator 215 is to allow intermittent operation of lift pump 212 to gain an average pump input power reduction over continuous operation.

While the first direct injection fuel rail 250 is coupled to the outlet 208 of HPP 214 (and not to the inlet of HPP 214), second port injection fuel rail 260 is coupled to the inlet 203 of HPP 214 (and not to the outlet of HPP 214). Although inlets, outlets, and the like relative to compression chamber 205 are described herein, it may be appreciated that there may be a single conduit into compression chamber 205. The single conduit may serve as inlet and outlet. In particular, second fuel rail 260 is coupled to HPP inlet 203 at a location upstream of solenoid activated control valve 236 and downstream of check valve 234 and pressure relief valve 232. Further, no additional pump may be required between lift pump 212 and the port injection fuel rail 260. As elaborated below, the specific configuration of the fuel system with the port injection fuel rail coupled to the inlet of the high pressure pump via a pressure relief valve and a check valve enables the pressure at the second fuel rail to be raised via the high pressure pump to a fixed default pressure that is above the default pressure of the lift pump. That is, the fixed high pressure at the port injection fuel rail is derived from the high pressure piston pump.

When the high pressure pump 214 is not reciprocating, such as at key-up before cranking, check valve 244 allows the second fuel rail to fill at 5 bar. As the pump chamber displacement becomes smaller due to the piston moving upward, the fuel flows in one of two directions. If the spill valve 236 is closed, the fuel goes into the high pressure fuel rail 250. If the spill valve 236 is open, the fuel goes either into the low pressure fuel rail 250 or through the compression relief valve 232. In this way, the high pressure fuel pump is operated to deliver fuel at a variable high pressure (such as between 15-200 bar) to the direct fuel injectors 252 via the first fuel rail 250 while also delivering fuel at a fixed high pressure (such as at 15 bar) to the port fuel injectors 262 via the second fuel rail 260. The variable pressure may include a minimum pressure that is at the fixed pressure (as in the system of FIG. 2). In the configuration depicted at FIG. 2, the fixed pressure of the port injection fuel rail is the same as the minimum pressure for the direct injection fuel rail, both being higher than the default pressure of the lift pump. Herein, the fuel delivery from the high pressure pump is controlled via the upstream (solenoid activated) control valve and further via the various check valve and pressure relief valves coupled to the inlet of the high pressure pump. By adjusting operation of the solenoid activated control valve, the fuel pressure at the first fuel rail is raised from the fixed pressure to the variable pressure while maintaining the fixed pressure at the second fuel rail. Valves 244 and 242 work in conjunction to keep the low pressure fuel rail 260 pressurized to 15 bar during the pump inlet stroke. Pressure relief valve 242 simply limits the pressure that can build in fuel rail 250 due to thermal expansion of fuel. A typical pressure relief setting may be 20 bar.

Controller 12 can also control the operation of each of fuel pumps 212, and 214 to adjust an amount, pressure, flow rate, etc., of a fuel delivered to the engine. As one example, controller 12 can vary a pressure setting, a pump stroke amount, a pump duty cycle command and/or fuel flow rate of the fuel pumps to deliver fuel to different locations of the fuel system. A driver (not shown) electronically coupled to controller 222 may be used to send a control signal to the low pressure pump, as required, to adjust the output (e.g. speed) of the low pressure pump.

The embodiment depicted at FIG. 2, and also at embodiment 300 of FIG. 3, show a first fuel system configuration wherein fuel is supplied to the port injection fuel rail from the fuel tank by branching off before the high pressure direct injection fuel pump (HPFP). It will be appreciated, however, that in alternate embodiments, such as shown at embodiment 350 of FIG. 3, fuel may be supplied to the port injection fuel rail from the fuel tank via the high pressure direct injection fuel pump.

In earlier engine fuel system configurations (e.g., prior art), a dedicated low pressure pump was used for pressurizing the port injection fuel rail, the low pressure pump distinct from the high pressure pump used for pressurizing the direct injection fuel rail. The present configurations, depicted at FIGS. 2-3, allow for hardware reduction by using the same pump to pressurize both fuel rails. However in both configurations, fuel flow through the HPFP can cause fuel pulsations to enter the port injection fuel rail. This is due to the high pressure piston pump being driven by an engine camshaft, resulting in a defined number of pulses being experienced at the HPFP, and thereby in the port injection fuel rail, on each engine rotation (e.g., 3 pulses every 270 degrees on a 4-cylinder in-line engine). The port injection fuel rail pulsations may be exacerbated during conditions when the high pressure fuel pump is not supplying fuel to the direct injection fuel rail (such as when no direct injection of fuel is requested) and when fuel is only being supplied to the port injection fuel rail (such as when only port injection of fuel is requested). This is due to the direct injection fuel rail returning all of the ingested volume of fuel back to the lower pressure system. These pulsations in the port injection fuel rail can lead to significant fueling errors.

As elaborated herein, the fueling errors may be reduced by adjusting the timing of a port injection fuel pulse. The delivery of the port injection pulse may be moved to coincide with an average pressure-crossing of the waveform (e.g., sinusoidal curve) of the port injection fuel rail's pressure (as shown at FIGS. 4-6B). In this way, fueling errors due to positive pressure excursions are cancelled by fueling errors due to negative pressure excursions, improving port fuel injection metering.

Turning now to method 400, an example method is shown for pressurizing fuel in a port injection fuel rail via an engine camshaft driven high pressure fuel pump and injecting a port fuel injection with a timing balanced around an average pressure-crossing of port fuel injection pressure. Instructions for carrying out method 400 and the rest of the methods included herein may be executed by a controller based on instructions stored on a memory of the controller and in conjunction with signals received from sensors of the engine system, such as the sensors described above with reference to FIGS. 1-3. The controller may employ engine actuators of the engine system to adjust engine operation, according to the methods described below.

At 402, the method includes estimating and/or measuring engine operating conditions. The parameters may include, for example, engine speed, driver torque demand, fuel rail pressure, engine temperature, ambient conditions, etc. At 404, the method includes determining a fuel injection profile based on the estimated engine operating conditions. The determined fuel injection profile may include an amount of fuel to be delivered via port injection (a port injection fuel pulse) and an amount of fuel to be delivered via direct injection (a direct injection fuel pulse). As an example, a desired fuel mass may be determined based on driver demand. Based on the desired fuel mass (for port and direct injection), and further based on fuel rail pressure, corresponding fuel pulses (for port and direct injection) may be calculated.

At 406, it may be confirmed that port injection was requested. If at least some port injection was requested, the method proceeds to 408. If no port injection is requested, and only direct injection (DI) is requested, the method moves to 424. Therein, only the direct injection fuel rail is pressurized via a high pressure fuel pump that is coupled to the engine and driven via the engine camshaft. Specifically, an output of the high pressure fuel pump is adjusted to provide the desired fuel rail pressure at the direct injection fuel rail. At 426, the method further includes calculating a DI fuel pulse width and timing based on the desired DI fuel mass. At 428, the method includes delivering the desired DI fuel mass by operating the high pressure fuel pump and injecting fuel via the direct injector with the determined DI fuel pulse width and timing.

If at least some port fuel injection (PFI) was requested at 406, the routine includes pressurizing fuel in the port injection fuel rail via the camshaft-driven high pressure fuel pump. This includes conditions where only port fuel injection is requested as well as conditions where port and direct fuel injection are both requested. Specifically, an output of the high pressure fuel pump is adjusted to provide the desired fuel rail pressure at the port injection fuel rail. At 410, a PFI fuel injection pulse width is calculated based on engine operating conditions, such as desired fuel mass and PFI fuel rail pressure. In one example, the port injection fuel rail pressure may be estimated by a pressure sensor coupled to the PFI fuel rail. In an alternate example, the port injection fuel rail pressure may be estimated based on each of fuel pressure at the high pressure fuel pump and a fuel pulse delay, the delay based on engine speed, as elaborated herein at FIGS. 6A-6B.

Specifically, map 600 of FIG. 6A shows a waveform of fuel pressure at the HPFP at plot 602 (dashed line, FP_HPFP). The fuel pressure at the HPFP may be measured by a pressure sensor coupled to the HPFP. A fuel pulse delay 604 may be applied to the fuel pressure at the HPFP and used to estimate the fuel pressure in the port injection fuel rail, depicted at plot 606 (solid line, FP_PFIFR). The fuel pulse delay represents a delay in the travel of a pulse of fuel from the HPFP into the PFI fuel rail. In the depicted example, the delay is represented as a duration elapsed from detection of a local maxima of a wave cycle in the fuel pressure at the HPFP to detection of the same local maxima in the fuel pressure of the PFI fuel rail. As such, the delay is based on engine speed, their relationship depicted at plot 650 of FIG. 6B. In particular, the delay is increased as the engine speed increases.

Returning to FIG. 4, at 412, the controller may calculate an initial timing for the port fuel injection based on the engine operating conditions and the fuel pulse width. The initial timing may be based on the velocity of the fuel travelling to the fuel rail from the HPFP, as well as a timing (or engine position) corresponding to intake valve opening. For example, the controller may calculate an initial end of injection angle for the PFI fuel pulse based on the fuel pulse width and the desired timing. In one example, the initial timing may correspond to a timing that allows for closed intake valve injection of the determined fuel mass. The initial timing may correspond to an engine position and may include a defined number of crank angle degrees. At 414, the method includes calculating a middle of injection angle for the PFI fuel pulse based on the initial end of injection angle timing and the fuel pulse width.

As such, the initial timing corresponding to closed intake valve injection may occur at any position of the waveform of the port injection fuel pressure, such as at or near a local maxima or a local minima. However, such locations may result in pressure fluctuations and thereby fueling errors. As elaborated herein, the controller may be configured to adjust the delivery of the port injection fuel pulse to inject the port fuel injection with an updated timing that is balanced around an average pressure-crossing of the estimated port injection fuel pressure. This allows fueling errors to be reduced.

Specifically, at 416, the method includes identifying a nearest average pressure crossing of port injection fuel pressure in the advanced direction. The average pressure-crossing may include an average pressure between a local maxima and a local minima (for a cycle of the pressure waveform) of port injection fuel pressure. In other words, for a sinusoidal pressure waveform, the average pressure-crossing may correspond to a timing where above-average pressure is cancelled by under-average pressure. The average pressure-crossing timing may be with reference to an engine position and may include a defined number of engine crank angle degrees. In one example, the average pressure-crossing includes a zero-crossing of port fuel injection pressure. As such, for every cycle of the waveform, there are two average pressure-crossings (or zero-crossings). The controller may identify and select a first average pressure-crossing in the advanced direction even if a second average pressure-crossing in the retarded direction is closer. By selecting the first average pressure-crossing in the advanced direction, closed intake valve injection of fuel can be maintained.

At 418, the method includes moving delivery of the port fuel injection pulse from the initial timing corresponding to closed intake valve injection to the first average pressure crossing in the advanced direction. In other words, delivery of the port fuel injection pulse is not moved to a second average pressure crossing in the retarded direction, even if a distance between the initial timing and the second average pressure crossing is smaller than the distance between the initial timing and the first average pressure crossing. The moving specifically includes aligning the middle of injection angle of the port injection fuel pulse (as determined for the initial timing) with the first average pressure crossing in the advanced direction.

At 420, the method includes adjusting intake port fuel puddle model dynamics based on the moving. In one example, due to the advancing of the timing, the adjusting may be performed to account for increased vaporization of fuel in the intake port due to a longer duration of the intake port fuel puddle sitting on the intake valve or on valve walls. Accordingly, the adjusting may include updating the fuel pulse width and moving an end of injection angle of the port injection fuel pulse based on the aligning of the middle of injection angle and the adjusted intake port fuel puddle model dynamics. As an example, to account for the increased vaporization of fuel in the intake port, the fuel pulse width may be shortened by maintaining the middle of injection angle at the average pressure-crossing while advancing the end of injection angle. A trimming factor may be determined based on the updated fuel pulse width relative to the initial fuel pulse width (as determined at 410), and the trimming factor may be applied to the end of injection angle.

It will be appreciated that injecting the port fuel injection with a timing balanced around an average pressure-crossing of port fuel injection pressure may include injecting each fuel injection pulse in a selected engine speed-load region with the timing balanced around the average pressure-crossing, while injecting each fuel injection pulse outside the selected engine speed-load region with a timing based on intake valve opening. Herein, the timing based on intake valve opening may include a timing offset from the average pressure-crossing (e.g., offset from the average pressure-crossing and towards the local maxima or a local minima of a cycle of the pressure waveform).

At 422, the method includes delivering or injecting fuel via the port injector according to the updated fuel pulse timing, and updated fuel pulse width, where applicable. If direct fuel injection was also requested along with the port fuel injection, the method may further include determining the pulse width add timing of the DI fuel pulse, and also delivering fuel via the direct injector according to the determined DI fuel pulse profile.

In this way, port fueling errors induced by pressure fluctuations at the HPFP are reduced. An example delivery of fuel via port fuel injection at an average pressure-crossing of port fuel injection pressure is now discussed with reference to FIG. 5.

Map 500 of FIG. 5 depicts a port injection fuel rail pressure at plot 502, and a port fuel injector duty cycle (PDI_DutyCycle) at plot 520. All plots are shown over time, depicted herein in terms of engine position in crank angle degrees (CAD).

As shown by the sinusoidal waveform of plot 502, the port injection fuel rail pressure may periodically fluctuate between a local maxima 504 and a local minima 506. A statistical average of the local maxima and the local minima is determined as the average pressure (P_average), shown here as a dashed line. The average pressure-crossings (herein also referred to as a zero-crossing) of the port injection fuel rail pressure, representing positions of the waveform that overlap with the average pressure, are represented by solid dots 508. As such, for each waveform cycle 505 (from one local minima to a subsequent local minima, as depicted, or from one local maxima to a subsequent local maxima), there may be two average pressure crossings 508 including one average pressure crossing on the ascending limb of the waveform (also referred to herein as an upward average pressure-crossing or upward zero-crossing) and one average pressure crossing on the decending limb of the waveform (also referred to herein as an downward average pressure-crossing or downward zero-crossing). It will be appreciated that while the waveform of FIG. 5 shows symmetric waves of equal intensity and a fixed frequency, in alternate examples, the waveform may be asymmetric such that the local maxima, minima, and average pressures for the waveform of each cycle are different from those of another cycle. In the depicted example, a first port injection fuel pulse PW0 is determined initially for port injection of fuel in a first cylinder, and a second port injection fuel pulse PW1 is determined initially for port injection of fuel in a second cylinder, the second cylinder firing immediately after the first cylinder. First fuel pulse PW0 may have an initial pulse width W0 and an initial timing 511 corresponding to a position at or around the local maxima. Second fuel pulse PW1 may have an initial pulse width W1 and an initial timing 513 corresponding to a position at or around the local minima.

To reduce fueling errors induced by the sinusoidal fuel pressure change, the duty cycle of the first port injection fuel pulse PW0 is adjusted to move the timing to be balanced around a first average pressure-crossing in the advanced direction relative to initial timing 511. Specifically, a middle of injection angle of first fuel pulse PW0 is moved from initial timing 511 and repositioned to be aligned with a first average pressure-crossing 508 a in the advanced direction. Herein, the first average pressure-crossing in the advanced direction is an upward pressure-crossing. Thus, initial first fuel pulse PW0 (dotted line) is repositioned, as shown by arrow 510, to updated first fuel pulse PW0′ (solid line). As a result of the repositioning, fueling errors caused by over-average pressure estimation can be cancelled by fueling errors caused by under average-pressure estimation (as shown by straight lines in PW0′ that are centered around 508 a). The repositioning is performed without the need for additional adjustments to the fuel pulse width. Thus, after the repositioning, updated first fuel pulse PW0′ has the same pulse width w1 as initial first fuel pulse PW0.

Also to reduce fueling errors induced by the sinusoidal fuel pressure change, the duty cycle of the second port injection fuel pulse PW1 is adjusted to move the timing to be balanced around a first average pressure-crossing in the advanced direction relative to initial timing 513. Specifically, a middle of injection angle of second fuel pulse PW1 is moved from initial timing 513 and repositioned to be aligned with a first average pressure-crossing 508 b in the advanced direction. Herein, the first average pressure-crossing 508 b in the advanced direction is a downward pressure-crossing. Herein, even though the initial timing 513 is significantly closer to second (upward) average pressure-crossing 508 c, due to second average pressure-crossing 508 c being in a retarded direction relative to initial timing 513, it is not selected. This allows closed intake valve port injection of fuel to be maintained. Instead, initial second fuel pulse PW1 (dotted line) is repositioned, as shown by arrow 512, to updated second fuel pulse PW1′ (solid line). As a result of the repositioning, fueling errors caused by over-average pressure estimation can be cancelled by fueling errors caused by under average-pressure estimation (as shown by straight lines in PW1′ that are centered around 508 b). The repositioning is performed with the need for additional adjustments to the fuel pulse width. Specifically, to compensate for the additional duration that the fuel sits at or near the closed intake valve, and the resultant increase in fuel vapor generation, after the repositioning, updated second fuel pulse PW1′ has a smaller pulse width w2′ as compared to the pulse width w2 of initial second fuel pulse PW1. Herein, this is achieved by aligning the middle of injection angle of PW1 with average-pressure crossing 508 b and then advancing the end of injection angle of PW1′ towards average-pressure crossing 508 b.

One example method for an engine comprises: pressurizing fuel in a port injection fuel rail via an engine camshaft driven high pressure fuel pump; and injecting a port fuel injection with a timing balanced around an average pressure-crossing of port fuel injection pressure. In the preceding example, additionally or optionally, the average pressure crossing includes a zero-crossing of port fuel injection pressure. In any or all of the preceding examples, additionally or optionally, the average pressure crossing of port fuel injection pressure includes an average pressure between a local maxima and a local minima of port fuel injection pressure. In any or all of the preceding examples, additionally or optionally, the injecting includes moving delivery of a port injection fuel pulse from an initial timing corresponding to closed intake valve injection to a first average pressure crossing in an advanced direction. In any or all of the preceding examples, additionally or optionally, the injecting further includes not moving delivery of the port injection fuel pulse to a second average pressure crossing in a retarded direction. In any or all of the preceding examples, additionally or optionally, the moving includes aligning a middle of injection angle of the port injection fuel pulse with the first average pressure crossing in the advanced direction. In any or all of the preceding examples, additionally or optionally, the method further comprises adjusting intake port fuel puddle model dynamics based on the moving. In any or all of the preceding examples, additionally or optionally, the method further comprises moving an end of injection angle of the port injection fuel pulse based on the aligning of the middle of injection angle and the adjusted intake port fuel puddle model dynamics. In any or all of the preceding examples, additionally or optionally, the injecting includes injecting each fuel injection pulse in a selected engine speed-load region with the timing balanced around the average pressure-crossing, the method further comprising, injecting each fuel injection pulse outside the selected engine speed-load region with a timing based on intake valve opening, the timing based on intake valve opening including a timing offset from the average pressure-crossing. In any or all of the preceding examples, additionally or optionally, the port fuel injection pressure is estimated based on each of fuel pressure at the high pressure fuel pump and a fuel pulse delay, the delay based on engine speed, the delay increased as the engine speed increases.

Another example method for an engine comprises: pressurizing fuel in a port injection fuel rail via an engine camshaft driven high pressure fuel pump; and moving a port injection fuel pulse from an initial timing based on intake valve opening to a final timing based on an estimated fuel pressure of the port injection fuel rail. In the preceding example, additionally or optionally, the estimated fuel pressure of the port injection fuel rail is based on a measured fuel pressure of the high pressure fuel pump. In any or all of the preceding examples, additionally or optionally, the high pressure fuel pump is a piston pump, and the estimated fuel pressure of the port injection fuel rail has a waveform, wherein a local maxima of the waveform is based on a fuel pressure of the high pressure fuel pump measured when the piston is at top dead center and a local minima of the waveform is based on the fuel pressure of the high pressure fuel pump measured when the piston is at bottom dead center. In any or all of the preceding examples, additionally or optionally, the estimated fuel pressure of the port injection fuel rail is further based on a fuel pulse delay between fuel at the high pressure fuel pump and fuel at the port injection fuel rail, the fuel pulse delay based on engine speed, the delay increased as the engine speed increases. In any or all of the preceding examples, additionally or optionally, the moving includes moving to a final timing that coincides with a first zero-crossing of the waveform in an advanced direction, and not to a second zero-crossing of the waveform in a retarded direction, the first and second zero-crossings corresponding to a mid-point between the local maxima and the local minima of the waveform. In any or all of the preceding examples, additionally or optionally, during a first condition, the first zero-crossing is an upward zero-crossing across the waveform while the second zero-crossing is a downward zero-crossing across the waveform, while during a second condition, the first zero-crossing is a downward zero-crossing across the waveform while the second zero-crossing is an upward zero-crossing across the waveform. In any or all of the preceding examples, additionally or optionally, the moving includes aligning a middle of injection angle of the port injection fuel pulse with the first zero-crossing. In any or all of the preceding examples, additionally or optionally, the moving further includes adjusting a beginning and end angle of the fuel pulse based on the aligning of the middle of injection angle. In any or all of the preceding examples, additionally or optionally, the method further comprises updating modeled puddle dynamics of an intake port fuel puddle based on the moving, and adjusting a pulse width of the port injection fuel pulse based on the updated model, the pulse width adjusted by adjusting an end of injection angle of the port injection fuel pulse. In any or all of the preceding examples, additionally or optionally, each of the initial and final timing include engine crank angle degrees (that is, they are related to an engine position). In any or all of the preceding examples, additionally or optionally, the method further comprises operating a port fuel injector to deliver the port injection fuel pulse at the final timing, and if direct injection is requested, pressurizing fuel in a direct injection fuel rail via the engine camshaft driven high pressure fuel pump.

Another example method for an engine comprises: pressurizing each of a port injection fuel rail and a direct injection fuel rail via an engine-driven high pressure piston fuel pump; and advancing a timing of a port injection fuel pulse based on a fuel pressure at the pump when the piston is at top dead center and a fuel pressure at the pump when the piston is at bottom dead center. In the preceding example, additionally or optionally, the advancing includes estimating a local maxima for a given pressure cycle in the port injection fuel rail based on a fuel pressure in the fuel pump when the piston is at TDC; estimating a local minima for the given pressure cycle in the port injection fuel rail based on the fuel pressure in the fuel pump when the piston is at BDC; estimating an average pressure in the port injection fuel rail based on the local maxima and local minima; and advancing the timing of an injection pulse to coincide with a timing of the average pressure.

In a further representation, an engine fuel system comprises: an engine; a first fuel rail coupled to a direct injector; a second fuel rail coupled to a port injector; a high pressure mechanical fuel pump driven by the engine via a camshaft, the fuel pump delivering fuel to each of the first and second fuel rails, the first fuel rail coupled to an outlet of the high pressure fuel pump, the second fuel rail coupled to an inlet of the high pressure fuel pump; a pressure sensor coupled to the fuel pump for estimating a fuel pressure at the fuel pump; an engine speed sensor; and a controller. The controller may be configured with computer readable instructions stored on non-transitory memory for: pressurizing the port injection fuel rail via the high pressure fuel pump; calculating fuel pressure in the second fuel rail based on the estimated fuel pressure at the fuel pump and estimated engine speed; determining an initial port fuel injection profile including an initial injection timing based on engine operating conditions; calculating each of a local maxima, a local minima, and an average pressure-crossing for one or more pressure cycles in the second fuel rail around the initial injection timing; and delivering fuel via the port injector at a final timing balanced around an average pressure-crossing advanced from the initial injection timing.

In another representation, a method for an engine comprises: pressurizing a port injection fuel rail and a direct injection fuel rail via an engine-driven high pressure piston fuel pump; estimating a local maxima for a given pressure cycle in the port injection fuel rail based on a fuel pressure in the fuel pump when the piston is at TDC; estimating a local minima for the given pressure cycle in the port injection fuel rail based on the fuel pressure in the fuel pump when the piston is at BDC; estimating an average pressure in the port injection fuel rail based on the local maxima and local minima; and moving a timing of an injection pulse to coincide with a timing of the average pressure. In the above embodiment, the moving includes advancing the timing of the injection pulse to coincide with a timing of the average pressure.

In this way, a PFI fuel pulse center is adjusted around an average pressure-crossing (e.g., a zero-crossing) of a fuel rail pressure to reduce metering errors. By aligning the middle of injection angle of the port injection fuel pulse to coincide with a first average pressure-crossing in the advanced direction, closed intake valve port fuel injection is enabled with fueling errors caused by over-pressure estimation to be cancelled by fueling errors caused by under-pressure estimation. By aligning the fuel pulse center with a position where the port injection fuel rail pressure fluctuates the least, the need for fast fuel pressure sampling while also reducing the dependence on hardware or software related to pressure dampening. Overall, metering of fuel from the port injection fuel rail is improved. By reducing fueling errors in fuel systems where a single high pressure pump can advantageously pressurize both direct and port injection rails, component reduction benefits are achieved without incurring a loss in fueling accuracy.

Note that the example control and estimation routines included herein can be used with various engine and/or vehicle system configurations. The control methods and routines disclosed herein may be stored as executable instructions in non-transitory memory and may be carried out by the control system including the controller in combination with the various sensors, actuators, and other engine hardware. The specific routines described herein may represent one or more of any number of processing strategies such as event-driven, interrupt-driven, multi-tasking, multi-threading, and the like. As such, various actions, operations, and/or functions illustrated may be performed in the sequence illustrated, in parallel, or in some cases omitted. Likewise, the order of processing is not necessarily required to achieve the features and advantages of the example embodiments described herein, but is provided for ease of illustration and description. One or more of the illustrated actions, operations and/or functions may be repeatedly performed depending on the particular strategy being used. Further, the described actions, operations and/or functions may graphically represent code to be programmed into non-transitory memory of the computer readable storage medium in the engine control system, where the described actions are carried out by executing the instructions in a system including the various engine hardware components in combination with the electronic controller.

It will be appreciated that the configurations and routines disclosed herein are exemplary in nature, and that these specific embodiments are not to be considered in a limiting sense, because numerous variations are possible. For example, the above technology can be applied to V-6, I-4, I-6, V-12, opposed 4, and other engine types. The subject matter of the present disclosure includes all novel and non-obvious combinations and sub-combinations of the various systems and configurations, and other features, functions, and/or properties disclosed herein.

The following claims particularly point out certain combinations and sub-combinations regarded as novel and non-obvious. These claims may refer to “an” element or “a first” element or the equivalent thereof. Such claims should be understood to include incorporation of one or more such elements, neither requiring nor excluding two or more such elements. Other combinations and sub-combinations of the disclosed features, functions, elements, and/or properties may be claimed through amendment of the present claims or through presentation of new claims in this or a related application. Such claims, whether broader, narrower, equal, or different in scope to the original claims, also are regarded as included within the subject matter of the present disclosure. 

1. A method for an engine, comprising: pressurizing fuel in a port injection fuel rail via an engine camshaft driven high pressure fuel pump; and injecting a port fuel injection with a timing balanced around an average pressure-crossing of port fuel injection pressure.
 2. The method of claim 1, wherein the average pressure crossing includes a zero-crossing of port fuel injection pressure.
 3. The method of claim 1, wherein average pressure crossing of port fuel injection pressure includes an average pressure between a local maxima and a local minima of port fuel injection pressure.
 4. The method of claim 1, wherein the injecting includes moving delivery of a port injection fuel pulse from an initial timing corresponding to closed intake valve injection to a first average pressure crossing in an advanced direction.
 5. The method of claim 4, wherein the injecting further includes not moving delivery of the port injection fuel pulse to a second average pressure crossing in a retarded direction.
 6. The method of claim 4, wherein the moving includes aligning a middle of injection angle of the port injection fuel pulse with the first average pressure crossing in the advanced direction.
 7. The method of claim 6, further comprising, adjusting intake port fuel puddle model dynamics based on the moving.
 8. The method of claim 7, further comprising, moving an end of injection angle of the port injection fuel pulse based on the aligning of the middle of injection angle and the adjusted intake port fuel puddle model dynamics.
 9. The method of claim 1, wherein the injecting includes injecting each fuel injection pulse in a selected engine speed-load region with the timing balanced around the average pressure-crossing, the method further comprising, injecting each fuel injection pulse outside the selected engine speed-load region with a timing based on intake valve opening, the timing based on intake valve opening including a timing offset from the average pressure-crossing.
 10. The method of claim 1, wherein the port fuel injection pressure is estimated based on each of fuel pressure at the high pressure fuel pump and a fuel pulse delay, the delay based on engine speed, the delay increased as the engine speed increases.
 11. A method for an engine, comprising: pressurizing fuel in a port injection fuel rail via an engine camshaft driven high pressure fuel pump; and moving a port injection fuel pulse from an initial timing based on intake valve opening to a final timing based on an estimated fuel pressure of the port injection fuel rail.
 12. The method of claim 11, wherein the high pressure fuel pump is a piston pump, wherein the estimated fuel pressure of the port injection fuel rail is based on a measured fuel pressure of the high pressure fuel pump, and wherein the estimated fuel pressure of the port injection fuel rail has a waveform, a local maxima of the waveform based on a fuel pressure of the high pressure fuel pump measured when the piston is at top dead center, a local minima of the waveform based on the fuel pressure of the high pressure fuel pump measured when the piston is at bottom dead center.
 13. The method of claim 12, wherein the estimated fuel pressure of the port injection fuel rail is further based on a fuel pulse delay between fuel at the high pressure fuel pump and fuel at the port injection fuel rail, the fuel pulse delay based on engine speed, the delay increased as the engine speed increases.
 14. The method of claim 12, wherein the moving includes moving to a final timing that coincides with a first zero-crossing of the waveform in an advanced direction, and not to a second zero-crossing of the waveform in a retarded direction, the first and second zero-crossings corresponding to a mid-point of the local maxima and the local minima.
 15. The method of claim 14, wherein during a first condition, the first zero-crossing is an upward zero-crossing across the waveform while the second zero-crossing is a downward zero-crossing across the waveform, and during a second condition, the first zero-crossing is a downward zero-crossing across the waveform while the second zero-crossing is an upward zero-crossing across the waveform.
 16. The method of claim 14, wherein the moving further includes aligning a middle of injection angle of the port injection fuel pulse with the first zero-crossing, and adjusting a beginning and end angle of the fuel pulse based on the aligning of the middle of injection angle.
 17. The method of claim 16, further comprising, updating modeled puddle dynamics of an intake port fuel puddle based on the moving, and adjusting a pulse width of the port injection fuel pulse based on the updated model, the pulse width adjusted by adjusting an end of injection angle of the port injection fuel pulse.
 18. The method of claim 12, wherein each of the initial and final timing include engine crank angle degrees, the method further comprising, operating a port fuel injector to deliver the port injection fuel pulse at the final timing, and if direct injection of fuel is requested, pressurizing fuel in a direct injection fuel rail via the engine camshaft driven high pressure fuel pump.
 19. A method for an engine comprising: pressurizing each of a port injection fuel rail and a direct injection fuel rail via an engine-driven high pressure piston fuel pump; and advancing a timing of a port injection fuel pulse based on a fuel pressure at the pump when the piston is at top dead center and a fuel pressure at the pump when the piston is at bottom dead center.
 20. The method of claim 19, wherein the advancing includes: estimating a local maxima for a given pressure cycle in the port injection fuel rail based on a fuel pressure in the fuel pump when the piston is at TDC; estimating a local minima for the given pressure cycle in the port injection fuel rail based on the fuel pressure in the fuel pump when the piston is at BDC; estimating an average pressure in the port injection fuel rail based on the local maxima and local minima; and advancing the timing of an injection pulse to coincide with a timing of the average pressure. 